WO2014062269A3 - Système de stabilisation d'un système électrique d'un aéronef - Google Patents

Système de stabilisation d'un système électrique d'un aéronef Download PDF

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Publication number
WO2014062269A3
WO2014062269A3 PCT/US2013/052596 US2013052596W WO2014062269A3 WO 2014062269 A3 WO2014062269 A3 WO 2014062269A3 US 2013052596 W US2013052596 W US 2013052596W WO 2014062269 A3 WO2014062269 A3 WO 2014062269A3
Authority
WO
WIPO (PCT)
Prior art keywords
secondary battery
aircraft
electric system
electric
stabilizing
Prior art date
Application number
PCT/US2013/052596
Other languages
English (en)
Other versions
WO2014062269A2 (fr
Inventor
Atsushi IWASHIMA
Kazushige Sugimoto
Kazuya Matsuo
Joseph S. BREIT
Farhad Nozari
Original Assignee
Kawasaki Jukogyo Kabushiki Kaisha
The Boeing Company
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Kawasaki Jukogyo Kabushiki Kaisha, The Boeing Company filed Critical Kawasaki Jukogyo Kabushiki Kaisha
Priority to CN201380039141.8A priority Critical patent/CN104471828B/zh
Priority to CA2871964A priority patent/CA2871964C/fr
Priority to EP13846974.7A priority patent/EP2880738B1/fr
Priority to BR112015001649-9A priority patent/BR112015001649B1/pt
Priority to US14/418,074 priority patent/US10279759B2/en
Priority to JP2015525496A priority patent/JP6251264B2/ja
Publication of WO2014062269A2 publication Critical patent/WO2014062269A2/fr
Publication of WO2014062269A3 publication Critical patent/WO2014062269A3/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R16/00—Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for
    • B60R16/02—Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for electric constitutive elements
    • B60R16/03—Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for electric constitutive elements for supply of electrical power to vehicle subsystems or for
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J4/00—Circuit arrangements for mains or distribution networks not specified as ac or dc
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D41/00—Power installations for auxiliary purposes
    • B64D41/007—Ram air turbines
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B13/00—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion
    • G05B13/02—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
    • G01R31/005—Testing of electric installations on transport means
    • G01R31/008—Testing of electric installations on transport means on air- or spacecraft, railway rolling stock or sea-going vessels
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
    • G01R31/40—Testing power supplies
    • G01R31/42—AC power supplies
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/50—On board measures aiming to increase energy efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • Artificial Intelligence (AREA)
  • Computer Vision & Pattern Recognition (AREA)
  • Evolutionary Computation (AREA)
  • Medical Informatics (AREA)
  • Software Systems (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)
  • Control Of Eletrric Generators (AREA)
  • Supply And Distribution Of Alternating Current (AREA)
  • Dc-Dc Converters (AREA)
  • Rectifiers (AREA)

Abstract

L'invention concerne un système électrique pour aéronef, comprenant un dispositif de stabilisation de puissance connecté à un bus ca primaire, et une batterie secondaire. La batterie secondaire a une tension nominale lui permettant d'absorber l'énergie de récupération issue d'un vérin de gouverne de commande. la charge/décharge de la batterie secondaire est commandée, sur la base d'une tension et d'une fréquence du bus ca primaire, pour stabiliser le système électrique.
PCT/US2013/052596 2012-07-30 2013-07-29 Système de stabilisation d'un système électrique d'un aéronef WO2014062269A2 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
CN201380039141.8A CN104471828B (zh) 2012-07-30 2013-07-29 用于飞机的电力系统稳定系统
CA2871964A CA2871964C (fr) 2012-07-30 2013-07-29 Systeme de stabilisation d'un systeme electrique d'un aeronef
EP13846974.7A EP2880738B1 (fr) 2012-07-30 2013-07-29 Système de stabilisation d'un système électrique d'un aéronef
BR112015001649-9A BR112015001649B1 (pt) 2012-07-30 2013-07-29 Sistema e método de estabilização de sistema elétrico para aeronave
US14/418,074 US10279759B2 (en) 2012-07-30 2013-07-29 System and method for stabilizing aircraft electrical systems
JP2015525496A JP6251264B2 (ja) 2012-07-30 2013-07-29 航空機用電気系統安定化システム

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/561,670 US20140032002A1 (en) 2012-07-30 2012-07-30 Electric system stabilizing system for aircraft
US13/561,670 2012-07-30

Publications (2)

Publication Number Publication Date
WO2014062269A2 WO2014062269A2 (fr) 2014-04-24
WO2014062269A3 true WO2014062269A3 (fr) 2014-07-03

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2013/052596 WO2014062269A2 (fr) 2012-07-30 2013-07-29 Système de stabilisation d'un système électrique d'un aéronef

Country Status (7)

Country Link
US (2) US20140032002A1 (fr)
EP (1) EP2880738B1 (fr)
JP (1) JP6251264B2 (fr)
CN (1) CN104471828B (fr)
BR (1) BR112015001649B1 (fr)
CA (1) CA2871964C (fr)
WO (1) WO2014062269A2 (fr)

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Also Published As

Publication number Publication date
EP2880738A2 (fr) 2015-06-10
CA2871964C (fr) 2017-10-31
US10279759B2 (en) 2019-05-07
CN104471828A (zh) 2015-03-25
WO2014062269A2 (fr) 2014-04-24
US20150165990A1 (en) 2015-06-18
JP2015533699A (ja) 2015-11-26
US20140032002A1 (en) 2014-01-30
CA2871964A1 (fr) 2014-04-24
BR112015001649A2 (pt) 2017-07-04
CN104471828B (zh) 2018-01-05
BR112015001649B1 (pt) 2021-12-07
EP2880738B1 (fr) 2018-05-30
EP2880738A4 (fr) 2016-04-27
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